Specification for internal retaining rings (imperial sizes)
€172.00
Specification for swaged cable-end assemblies (Unified threads) for preformed steel wire rope (W.9) for aircraft
€201.00
Specification for swaged cable-end assemblies (Unified threads) for preformed non-corrodible steel wire rope (W.11) for aircraft
Specifications for hydraulic surface-check type lubricating nipples for aircraft
Collars for shear pins for aircraft
Specification for corrosion resisting worm drive clamps for aircraft
Specification for chromium-molybdenum steel tube (700 MPa) (outside diameter not less than 12.5 mm) (weldable)
Specification for chromium-molybdenum steel tube (1150 MPa) (maximum thickness 8 mm)
Specification for 18/10 chromium-nickel corrosion-resisting steel tube (niobium stabilized: 550 MPa) (weldable)
€99.00
Specification for 18/10 chromium-nickel corrosion-resisting steel tube (titanium stabilized: 550 N/mm2) (weldable)
Specification for cold drawn 18/10 chromium-nickel corrosion-resisting steel tube (niobium stabilized: 800 MPa) (weldable)
Specification for cold drawn 18/10 chromium-nickel corrosion-resisting steel tube (titanium stabilized: 800 N/mm2) (weldable)
€80.00
Specification for chromium-molybdenum steel tube (770 MPa) (weldable)
Specification for chromium-molybdenum steel tube (900 MPa) (weldable)
Specification for aircraft material. Preformed corrosion-resisting steel wire rope
